On The Wing Of Speed

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High Speed Wing Theory

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Author : Doris Cohen
language : en
Publisher: Princeton University Press
Release Date : 2015-12-08

High Speed Wing Theory written by Doris Cohen and has been published by Princeton University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-12-08 with Technology & Engineering categories.

Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Aerodynamic Components Of Aircraft At High Speeds

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Author : Allen F. Donovan
language : en
Publisher: Princeton University Press
Release Date : 2015-12-08

Aerodynamic Components Of Aircraft At High Speeds written by Allen F. Donovan and has been published by Princeton University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-12-08 with Science categories.

Volume VII of the High Speed Aerodynamics and Jet Propulsion series. It deals with applications to specific components of the complete aircraft. Sections of the volume include: aerodynamics of wings at high speed, aerodynamics of bodies at high speed, interaction problems, propellers at high speed, diffusers and nozzles, and nonsteady wing characteristics. Originally published in 1957. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

On The Wing

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Author : Dr. David E. Alexander
language : en
Publisher: Oxford University Press, USA
Release Date : 2015

On The Wing written by Dr. David E. Alexander and has been published by Oxford University Press, USA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015 with Science categories.

"On the Wing is the first book to take a comprehensive look at the evolution of flight in all four groups of powered flyers: insects, pterosaurs, birds, and bats."--Book jacket.

The Influence Of Wing Setting On The Wing Load And Rotor Speed Of A Pca 2 Autogiro As Determined In Flight

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Author : John B. Wheatley
language : en
Publisher:
Release Date : 1935

The Influence Of Wing Setting On The Wing Load And Rotor Speed Of A Pca 2 Autogiro As Determined In Flight written by John B. Wheatley and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1935 with categories.

Low Speed Aerodynamics

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Author : Joseph Katz
language : en
Publisher: Cambridge University Press
Release Date : 2001-02-05

Low Speed Aerodynamics written by Joseph Katz and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001-02-05 with Technology & Engineering categories.

Low-speed aerodynamics is important in the design and operation of aircraft flying at low Mach number, and ground and marine vehicles. This 2001 book offers a modern treatment of the subject, both the theory of inviscid, incompressible, and irrotational aerodynamics and the computational techniques now available to solve complex problems. A unique feature of the text is that the computational approach (from a single vortex element to a three-dimensional panel formulation) is interwoven throughout. Thus, the reader can learn about classical methods of the past, while also learning how to use numerical methods to solve real-world aerodynamic problems. This second edition has a new chapter on the laminar boundary layer (emphasis on the viscous-inviscid coupling), the latest versions of computational techniques, and additional coverage of interaction problems. It includes a systematic treatment of two-dimensional panel methods and a detailed presentation of computational techniques for three-dimensional and unsteady flows. With extensive illustrations and examples, this book will be useful for senior and beginning graduate-level courses, as well as a helpful reference tool for practising engineers.

Low Speed Characteristics In Pitch Of A 340 Sweptforward Wing With Circular Arc Airfoil Sections

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Author : D. William Conner
language : en
Publisher:
Release Date : 1947

Low Speed Characteristics In Pitch Of A 340 Sweptforward Wing With Circular Arc Airfoil Sections written by D. William Conner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aerodynamics categories.

Span Loadings Due To Wing Twist At Transonic And Supersonic Speeds

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Author : Frederick C. Grant
language : en
Publisher:
Release Date : 1957

Span Loadings Due To Wing Twist At Transonic And Supersonic Speeds written by Frederick C. Grant and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamic load categories.

Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been tested in the Mach number range from 0.8 to 2.0. The test results showed, in general, rather good agreement with theoretical predictions of the incremental span loadings due to twist for zero angle of attack. The measured incremental span loadings due to twist generally diminished with increasing angle of attack through the Mach number range. At a Mach number of 0.9, the incremental loadings progressively vanished from the tip inboard with increasing angle of attack. For the highest angles of attack (about 20 degrees) at Mach number 0.9, there was no difference in the span loadings of the flat and twisted wings. At a higher supersonic speeds, a similar vanishing at the tips of the incremental loading due to twist was starting at the highest angles of attack (near 20 degrees).

Three Dimensional Unsteady Lift Problems In High Speed Flight

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Author : Harvard Lomax
language : en
Publisher:
Release Date : 1951

Three Dimensional Unsteady Lift Problems In High Speed Flight written by Harvard Lomax and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Airplanes categories.

The indicial lift and pitching-moment coefficients are derived for flat-plate triangular wings at supersonic speeds. Coefficients are determined for angle-of-attack distributions corresponding to sinking and pitching wings. The wing with supersonic edges is completely analyzed, the wing with subsonic edges is partially analyzed; the solution in this case being completed for very narrow wings by an application of slender wing theory. In case of the supersonic edges, a comparison is made with known two-dimensional results and also with results for the same triangular wing in reversed flow.

Low Speed Investigation Of The Effects Of Wing Sweep On The Aerodynamic Characteristics Of Parawings Having Equal Length Leading Edges And Keel

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Author : Rodger L. Naeseth
language : en
Publisher:
Release Date : 1963

Low Speed Investigation Of The Effects Of Wing Sweep On The Aerodynamic Characteristics Of Parawings Having Equal Length Leading Edges And Keel written by Rodger L. Naeseth and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aerodynamics categories.

An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodynamic characteristics of a related series of parawings in which wing sweep was the primary variable. The leading-edge sweep angles varied from 400 to 750 and the three basic parawings had flat-planform sweep angles of 350, 450, and 550. The canopies of the wings were made of fabric. Tests were made at an airspeed of 38.6 mph and a Reynolds number of approximately 1.5 X 106. The maximum angle-of-attack range was from 140 to 530 for the wings having a canopy of 350 flat-planform sweep. A limited investigation of lateral characteristics was made for sideslip angles from approximately -50 to 160 for two angles of attack, and lateral stability derivatives were obtained for some configurations through a angle-of-attack range. Forces and moments acting on the wing and apex hinge moments were measured.

The Speed Of Heat

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Author : Thomas W. Young
language : en
Publisher: McFarland
Release Date : 2010-03-22

The Speed Of Heat written by Thomas W. Young and has been published by McFarland this book supported file pdf, txt, epub, kindle and other format this book has been release on 2010-03-22 with History categories.

With its fleet of large transport aircraft, the United States military can put personnel and equipment anywhere on the globe within hours. In the Iraq and Afghanistan wars in particular, virtually every soldier, every bullet, every pint of blood, and every bite of food have arrived in the war zone by airlift. This book tells the story of one Air National Guard airlift wing as related by its members. The 167th Airlift Wing of the West Virginia Air National Guard consisted of a squadron of 12 C-130 cargo planes, their crews, and all the supporting sections--in all, more than 1,200 people. The author, a former Associated Press reporter turned aviator, flew as an active member of that unit and interviewed nearly 70 servicemen and women for this book. They include aircrews who dodged heat-seeking missiles, mechanics who made combat repairs, flight nurses who treated and transported the wounded, even two motor pool truck drivers struck by a roadside bomb.